US4156614A - Alumina-based ceramics for core materials - Google Patents
Alumina-based ceramics for core materials Download PDFInfo
- Publication number
- US4156614A US4156614A US05/839,990 US83999077A US4156614A US 4156614 A US4156614 A US 4156614A US 83999077 A US83999077 A US 83999077A US 4156614 A US4156614 A US 4156614A
- Authority
- US
- United States
- Prior art keywords
- alumina
- ceramic
- fired
- core
- ceramic material
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
- C04B35/10—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on aluminium oxide
- C04B35/111—Fine ceramics
- C04B35/113—Fine ceramics based on beta-aluminium oxide
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C1/00—Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
- C04B35/10—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on aluminium oxide
- C04B35/101—Refractories from grain sized mixtures
Definitions
- This invention relates to materials suitable for making cores for casting directionally solidified eutectic and superalloy materials.
- Jet engines are a multi-million dollar business. The maximum operating temperature of these engines must be increased to attain higher efficiencies. Higher operating temperatures require the fabrication of new alloys with high temperature strength, toughness and corrosion resistance.
- the most promising method of fabricating the turbine blade components with improved high temperature properties is by directional solidification (DS).
- DS directional solidification
- the rate of production of blades by the DS process is partly governed by the liquidus temperature which should be as high as possible.
- the liquidus temperature of many of the promising alloy compositions being explored at this time is greater than 1500° C. and reaches nearly 1800° C. or higher.
- the alloy is solidified around a ceramic core material which is subsequently leached away, leaving behind the proper air cooling cavities in the blade.
- fused silica is the standard core material used at temperatures up to about 1550° C. without deleterious reaction with many of the alloy compositions.
- silica cores are severely attached by one or more of the most reactive elements (A1, Hf, C) of the alloy. Consequently, silica cores cannot be used at the high temperatures required to directionally solidify the alloy. MgO and Y 2 O 3 cores are found to react only slightly with the aluminum in the alloy during DS at temperatures near 1800° C., but both materials have relatively poor leachabilities.
- leachability and nonreactivity with the alloy up to 1800° C. are the two primary characteristics of the core material, other desirable characteristics are that it (1) be economical, (2) not undergo more than an overall dimensional change of ⁇ 2-4%, (3) have a porosity of from about 25% to about 60% to aid degassing during DS and increase the rate of leachability, (4) exhibit a modulus of rupture of only about 100 psi so that good crushability of the core occurs after the metal is cast, and (5) have good thermal shock resistance.
- Another object of this invention is to provide a new and improved material composition for making ceramic cores which is also economical for use in casting directionally solidified eutectic alloys and superalloy materials.
- a further object of this invention is to provide a new and improved material composition for making ceramic cores having increased porosity, leachability and crushability characteristics.
- a fired ceramic compact suitable for use in a core in the casting and directional solidification of eutectic alloys and superalloy materials.
- the ceramic material is an alumina-based material such as ⁇ -alumina, Na 2 O . 9A1 2 O 3 - Na 2 O . 11Al 2 O 3 , and other choice candidate materials such as CaO . 6Al 2 O 3 , SrO . 6A1 2 O 3 and BaO . 6Al 2 O 3 .
- the ceramic material after firing is characterized by an interconnected network of porosity and solid phase.
- the density of the fired compact is from about 40% to about 75%.
- a desirable material composition can also be produced by admixing up to about 40 parts by weight of pure alumina to each of the alumina-based ceramic compounds and form in situ the interconnected network in which may be found a dispersion of particles of alumina within a matrix of alumina-based compounds.
- Cores made of alumina-based ceramics of this invention are easily removed from the cast metal by autoclave leaching techniques embodying solutions of KOH or NaOH.
- the ⁇ -aluminates, Na 2 O ⁇ 9Al 2 O 3 - Na 2 O ⁇ 11Al 2 O 3 are desirable for making the ceramic cores because of their excellent leaching characteristics.
- Alumina-based compounds such as Na 2 O ⁇ 9Al 2 O 3 - Na 2 O ⁇ 11Al 2 O 3 , CaO ⁇ 6Al 2 O 3 , SrO ⁇ 6Al 2 O 3 and BaO . 6Al 2 O 3 have been discovered to be suitable materials for use in making cores for use in casting directionally solidified eutectic alloy and superalloy materials. All of these materials have a minimum temperature at which a liquid phase forms between the compound and alumina (Al.sub. 2 O 3 ) which is greater than 1800° C. which is the predicted maximum temperature that will be imposed upon the ceramic core material during directional solidification.
- the alumina-based compounds may comprise at least in part the ceramic material composition used in preparing a ceramic core from the composition.
- the material composition may consist essentially of 100 parts by weight of an individual alumina-based compound. Alternately the composition may comprise a two phase mixture of from about 60 parts by weight to 100 parts by weight of the alumina-based compounds, balance alumina.
- a continuous phase of the alumina-based ceramic compound is formed in situ which provides either an interconnected network of solid and porous phases or a dispersion of particles of alumina within a porous matrix of alumina-based compounds.
- Fired compacts of any of these material compositions when employed as cores in the casting and directional solidification of eutectic and superalloy materials, are easily removed therefrom by a caustic autoclave processing technique. Removal is achieved by leaching away the interconnected network of the alumina-based ceramic compound with a caustic agent of either a KOH or a NaOH solution.
- Another particular feature of material compositions embodying two phase ceramic cores is that the activity of the alumina in the core is nearly equal to that of pure alumina.
- the activity of the other oxide constituent in the phase mixture such, for example as Na 2 O, is considerably reduced so as to decrease its volatility to decrease its possible reactivity with the superalloy melt.
- Cores made from material compositions including one or more of these sodium aluminates are leachable in a 20% KOH or NaOH aqueous solution at from 200° C. to 350° C. in an autoclave.
- the process is economical and fairly fast, the leaching rate being on the order of from 0.5 to 1.0 centimeters per hour.
- the material composition for core making is prepared by mixing the materials together mechanically. A sufficient amount of the material composition, with or without a binder material admixed therein, is placed in a mold and pressed to a green compact having a desired configuration. The green compact is fired at a temperature of from 1600° C. to 1800° C. to form the core whose material is characterized by a continuous phase of alumina-based ceramic compound formed in situ by sintering.
- the material structure is characterized by either an interconnected network of solid and porous phases or particles of alumina within a porous matrix of alumina-based compounds.
- the density of the fired compact varies with the particle size of the materials employed. For a range of particle size of from about 1 micron to about 50 microns, the density of the fired compact ranges from about 40 percent to about 75 percent.
- a core 8 cm + 0.6 cm was made of substantially 100 parts by weight ⁇ -alumina material (Na 2 O ⁇ 9A1 2 O 3 ).
- the average particle size of the material used was about 35 microns for a particle size distribution ranging between 5 and 50 microns.
- the compact was formed at a pressure of 10,000 psi and fired at 1800° C. ⁇ 10° C. to sinter the compact for ease of handling.
- the density of the sintered rod was 55 percent.
- a melt of NiTaC-13 alloy was prepared, cast about the rod and directionally solidified thereabout at a temperature of 1675° C. ⁇ 25° C. for 20 hours in a controlled atmosphere of 10% CO by volume of argon gas.
- the alloy composition, as cast was as follows:
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Mechanical Engineering (AREA)
- Compositions Of Oxide Ceramics (AREA)
- Mold Materials And Core Materials (AREA)
- Porous Artificial Stone Or Porous Ceramic Products (AREA)
- Ceramic Products (AREA)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/839,990 US4156614A (en) | 1977-10-06 | 1977-10-06 | Alumina-based ceramics for core materials |
JP9416878A JPS5455013A (en) | 1977-10-06 | 1978-08-03 | Ceramic based on coreemateriallgrade alumina |
EP78101012A EP0001434A1 (en) | 1977-10-06 | 1978-09-28 | Alumina-based ceramics for core materials |
IT28255/78A IT1099621B (it) | 1977-10-06 | 1978-09-29 | Ceramiche basate su allumina per materiali di anima da fonderia |
NO783375A NO783375L (no) | 1977-10-06 | 1978-10-05 | Keramisk materiale paa basis av aluminiumoxyd |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/839,990 US4156614A (en) | 1977-10-06 | 1977-10-06 | Alumina-based ceramics for core materials |
Publications (1)
Publication Number | Publication Date |
---|---|
US4156614A true US4156614A (en) | 1979-05-29 |
Family
ID=25281174
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US05/839,990 Expired - Lifetime US4156614A (en) | 1977-10-06 | 1977-10-06 | Alumina-based ceramics for core materials |
Country Status (5)
Country | Link |
---|---|
US (1) | US4156614A (it) |
EP (1) | EP0001434A1 (it) |
JP (1) | JPS5455013A (it) |
IT (1) | IT1099621B (it) |
NO (1) | NO783375L (it) |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4480681A (en) * | 1982-08-30 | 1984-11-06 | Doulton Industrial Products Limited | Refractory mould body and method of casting using the mould body |
US4837187A (en) * | 1987-06-04 | 1989-06-06 | Howmet Corporation | Alumina-based core containing yttria |
US4836268A (en) * | 1987-01-17 | 1989-06-06 | Rolls-Royce Plc | Method of enhancing the leaching rate of a given material |
WO1989005204A1 (en) * | 1987-12-08 | 1989-06-15 | Harri Sahari | Method for preparation of moulds and cores used in the casting of metals |
US5129998A (en) * | 1991-05-20 | 1992-07-14 | Reynolds Metals Company | Refractory hard metal shapes for aluminum production |
US5336645A (en) * | 1993-09-27 | 1994-08-09 | Corning Incorporated | Soluble, cellulated mold and foamable mixture |
US5409871A (en) * | 1993-11-02 | 1995-04-25 | Pcc Airfoils, Inc. | Ceramic material for use in casting reactive metals |
US5545003A (en) * | 1992-02-18 | 1996-08-13 | Allison Engine Company, Inc | Single-cast, high-temperature thin wall gas turbine component |
US5552356A (en) * | 1994-07-11 | 1996-09-03 | Bayer Ag | Boron subphosphide/aluminum oxide composite materials, processes for the production thereof and use thereof |
US5810552A (en) * | 1992-02-18 | 1998-09-22 | Allison Engine Company, Inc. | Single-cast, high-temperature, thin wall structures having a high thermal conductivity member connecting the walls and methods of making the same |
US6494250B1 (en) | 2001-05-14 | 2002-12-17 | Howmet Research Corporation | Impregnated alumina-based core and method |
US20050269055A1 (en) * | 1998-11-20 | 2005-12-08 | Frasier Donald J | Method and apparatus for production of a cast component |
US20060243421A1 (en) * | 2005-04-29 | 2006-11-02 | United States Of America, Represented By Secretary Of The U.S. Army | Soluble casting core for metal matrix composite components and method of producing thereof |
US20080135204A1 (en) * | 1998-11-20 | 2008-06-12 | Frasier Donald J | Method and apparatus for production of a cast component |
US10364189B2 (en) | 2017-05-04 | 2019-07-30 | General Electric Company | Methods for forming ceramic cores |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2042951B (en) * | 1978-11-08 | 1982-08-04 | Rolls Royce | Investment casting core |
JPS62153158A (ja) * | 1985-08-30 | 1987-07-08 | 東洋シーシーアイ株式会社 | 耐熱性触媒又は触媒担体及びその製造方法 |
US4771028A (en) * | 1985-08-30 | 1988-09-13 | Catalysts And Chemicals Inc. | Heat resistant composition and method of producing the same |
JPS63242917A (ja) * | 1987-03-27 | 1988-10-07 | Agency Of Ind Science & Technol | 耐熱性アルミナ複合酸化物の製造方法 |
GB8925289D0 (en) * | 1989-11-09 | 1989-12-28 | Lilliwyte Sa | Method of making analogues of beta"-alumina |
US5458868A (en) * | 1989-11-09 | 1995-10-17 | Lilliwyte Societe Anonyme | Method of making analogues of β-alumina |
US20160175923A1 (en) * | 2012-04-09 | 2016-06-23 | General Electric Company | Composite core for casting processes, and processes of making and using the same |
JP6366555B2 (ja) * | 2015-09-24 | 2018-08-01 | 日本特殊陶業株式会社 | スパークプラグ |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB618248A (en) * | 1945-04-10 | 1949-02-18 | Corning Glass Works | Cast refractory products |
US3078173A (en) * | 1960-11-08 | 1963-02-19 | Harbison Walker Refractories | Aluminum melting furnace refractory |
US3312558A (en) * | 1966-05-17 | 1967-04-04 | Jr Eldon D Miller | Calcium hexaluminate articles |
US3643728A (en) * | 1970-07-08 | 1972-02-22 | United Aircraft Corp | Process of casting nickel base alloys using water-soluble calcia cores |
JPS4920365A (it) * | 1972-05-20 | 1974-02-22 | ||
US3901733A (en) * | 1974-10-07 | 1975-08-26 | Trw Inc | Thin film solid electrolyte structures and process of making same |
US4052538A (en) * | 1976-04-19 | 1977-10-04 | General Motors Corporation | Method of making sodium beta-alumina powder and sintered articles |
US4068048A (en) * | 1975-03-20 | 1978-01-10 | Compagnie Generale D'electricite S.A. | Method for preparing alkaline beta alumina parts |
US4073662A (en) * | 1977-03-09 | 1978-02-14 | General Electric Company | Method for removing a magnesia doped alumina core material |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR484314A (fr) * | 1916-02-02 | 1917-09-25 | Edward Irwing Braddock | Perfectionnements aux pointes ou clous fabriqués avec du fil métallique |
DE1257050B (de) * | 1959-06-23 | 1967-12-21 | Harbison Walker Refractories | Gebrannter, feuerfester Formkoerper fuer die Auskleidung von metallurgischen Gefaessen, in denen fluessiges Aluminium gehandhabt wird |
GB1185725A (en) * | 1967-11-03 | 1970-03-25 | Ass Elect Ind | Beta-Alumina Polycrystalline Ceramics |
GB1287571A (en) * | 1968-08-05 | 1972-08-31 | English Electric Co Ltd | Ceramic materials |
BE758568A (fr) * | 1969-11-10 | 1971-05-06 | Aluminum Co Of America | Perfectionnement du procede de production de l'alumine beta |
BE791380A (fr) * | 1972-01-19 | 1973-03-01 | Buckbee Mears Co | Produits ceramiques et compositions ceramiques |
CA1065580A (en) * | 1975-05-02 | 1979-11-06 | Donald Pearlman | Methods for producing beta-alumina composites |
-
1977
- 1977-10-06 US US05/839,990 patent/US4156614A/en not_active Expired - Lifetime
-
1978
- 1978-08-03 JP JP9416878A patent/JPS5455013A/ja active Pending
- 1978-09-28 EP EP78101012A patent/EP0001434A1/en not_active Withdrawn
- 1978-09-29 IT IT28255/78A patent/IT1099621B/it active
- 1978-10-05 NO NO783375A patent/NO783375L/no unknown
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB618248A (en) * | 1945-04-10 | 1949-02-18 | Corning Glass Works | Cast refractory products |
US3078173A (en) * | 1960-11-08 | 1963-02-19 | Harbison Walker Refractories | Aluminum melting furnace refractory |
US3312558A (en) * | 1966-05-17 | 1967-04-04 | Jr Eldon D Miller | Calcium hexaluminate articles |
US3643728A (en) * | 1970-07-08 | 1972-02-22 | United Aircraft Corp | Process of casting nickel base alloys using water-soluble calcia cores |
JPS4920365A (it) * | 1972-05-20 | 1974-02-22 | ||
US3901733A (en) * | 1974-10-07 | 1975-08-26 | Trw Inc | Thin film solid electrolyte structures and process of making same |
US4068048A (en) * | 1975-03-20 | 1978-01-10 | Compagnie Generale D'electricite S.A. | Method for preparing alkaline beta alumina parts |
US4052538A (en) * | 1976-04-19 | 1977-10-04 | General Motors Corporation | Method of making sodium beta-alumina powder and sintered articles |
US4073662A (en) * | 1977-03-09 | 1978-02-14 | General Electric Company | Method for removing a magnesia doped alumina core material |
Cited By (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4480681A (en) * | 1982-08-30 | 1984-11-06 | Doulton Industrial Products Limited | Refractory mould body and method of casting using the mould body |
US4836268A (en) * | 1987-01-17 | 1989-06-06 | Rolls-Royce Plc | Method of enhancing the leaching rate of a given material |
US4837187A (en) * | 1987-06-04 | 1989-06-06 | Howmet Corporation | Alumina-based core containing yttria |
WO1989005204A1 (en) * | 1987-12-08 | 1989-06-15 | Harri Sahari | Method for preparation of moulds and cores used in the casting of metals |
GB2230269A (en) * | 1987-12-08 | 1990-10-17 | Harri Sahari | Method for preparation of moulds and cores used in the casting of metals |
GB2230269B (en) * | 1987-12-08 | 1991-05-15 | Harri Sahari | Method for preparation of moulds and cores used in the casting of metals |
US5129998A (en) * | 1991-05-20 | 1992-07-14 | Reynolds Metals Company | Refractory hard metal shapes for aluminum production |
US5924483A (en) * | 1992-02-18 | 1999-07-20 | Allison Engine Company, Inc. | Single-cast, high-temperature thin wall structures having a high conductivity member connecting the walls and methods of making the same |
US6255000B1 (en) | 1992-02-18 | 2001-07-03 | Allison Engine Company, Inc. | Single-cast, high-temperature, thin wall structures |
US5545003A (en) * | 1992-02-18 | 1996-08-13 | Allison Engine Company, Inc | Single-cast, high-temperature thin wall gas turbine component |
US6244327B1 (en) | 1992-02-18 | 2001-06-12 | Allison Engine Company, Inc. | Method of making single-cast, high-temperature thin wall structures having a high thermal conductivity member connecting the walls |
US6071363A (en) * | 1992-02-18 | 2000-06-06 | Allison Engine Company, Inc. | Single-cast, high-temperature, thin wall structures and methods of making the same |
US5641014A (en) * | 1992-02-18 | 1997-06-24 | Allison Engine Company | Method and apparatus for producing cast structures |
US5810552A (en) * | 1992-02-18 | 1998-09-22 | Allison Engine Company, Inc. | Single-cast, high-temperature, thin wall structures having a high thermal conductivity member connecting the walls and methods of making the same |
US5336645A (en) * | 1993-09-27 | 1994-08-09 | Corning Incorporated | Soluble, cellulated mold and foamable mixture |
US5580837A (en) * | 1993-11-02 | 1996-12-03 | Pcc Airfoils, Inc. | Ceramic material for use in casting reactive metals |
US5409871A (en) * | 1993-11-02 | 1995-04-25 | Pcc Airfoils, Inc. | Ceramic material for use in casting reactive metals |
US5552356A (en) * | 1994-07-11 | 1996-09-03 | Bayer Ag | Boron subphosphide/aluminum oxide composite materials, processes for the production thereof and use thereof |
US20080142186A1 (en) * | 1998-11-20 | 2008-06-19 | Frasier Donald J | Method and apparatus for production of a cast component |
US20050269055A1 (en) * | 1998-11-20 | 2005-12-08 | Frasier Donald J | Method and apparatus for production of a cast component |
US20080135204A1 (en) * | 1998-11-20 | 2008-06-12 | Frasier Donald J | Method and apparatus for production of a cast component |
US20080149295A1 (en) * | 1998-11-20 | 2008-06-26 | Frasier Donald J | Method and apparatus for production of a cast component |
US7779890B2 (en) | 1998-11-20 | 2010-08-24 | Rolls-Royce Corporation | Method and apparatus for production of a cast component |
US8082976B2 (en) | 1998-11-20 | 2011-12-27 | Rolls-Royce Corporation | Method and apparatus for production of a cast component |
US8844607B2 (en) | 1998-11-20 | 2014-09-30 | Rolls-Royce Corporation | Method and apparatus for production of a cast component |
US8851152B2 (en) | 1998-11-20 | 2014-10-07 | Rolls-Royce Corporation | Method and apparatus for production of a cast component |
US8851151B2 (en) | 1998-11-20 | 2014-10-07 | Rolls-Royce Corporation | Method and apparatus for production of a cast component |
US6494250B1 (en) | 2001-05-14 | 2002-12-17 | Howmet Research Corporation | Impregnated alumina-based core and method |
US20060243421A1 (en) * | 2005-04-29 | 2006-11-02 | United States Of America, Represented By Secretary Of The U.S. Army | Soluble casting core for metal matrix composite components and method of producing thereof |
US20070131374A1 (en) * | 2005-04-29 | 2007-06-14 | U.S. Government, Represented By Secretary Of The Army | Soluble Casting Core For Metal Matrix Composite Components and Method of Producing Thereof |
US10364189B2 (en) | 2017-05-04 | 2019-07-30 | General Electric Company | Methods for forming ceramic cores |
Also Published As
Publication number | Publication date |
---|---|
NO783375L (no) | 1979-04-09 |
JPS5455013A (en) | 1979-05-01 |
IT1099621B (it) | 1985-09-18 |
IT7828255A0 (it) | 1978-09-29 |
EP0001434A1 (en) | 1979-04-18 |
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